CN219884121U - Unmanned aerial vehicle shock absorber support for aerial survey remote sensing - Google Patents

Abstract

The utility model relates to the technical field of unmanned aerial vehicle equipment, and discloses an unmanned aerial vehicle shock absorbing support for aerial survey remote sensing, which comprises a main body, wherein a sliding rod is fixedly connected to the front edge of the outer surface of the upper end of the main body, a sliding block is slidingly connected to the outer surface of the upper end of the sliding rod, an upper support frame is fixedly connected to the center of the outer surface of the front end of the sliding block, a fixed shaft is movably connected to the middle of the outer surface of the front end of the upper support frame, and a first spring is fixedly connected to the inner surface of the front end of the upper support frame, which is close to the upper end. This unmanned aerial vehicle shock absorber support for aerial survey remote sensing possesses convenient operation, supports advantages such as size adjustable, anti-impact, has solved and to use to same size unmanned aerial vehicle only, and can not dismantle, is unfavorable for accomodating, and is inconvenient in the use, does not have shock-absorbing structure, when descending suddenly, because too big impact force leads to the interior part to damage, influences unmanned aerial vehicle's life's problem.

Description

Unmanned aerial vehicle shock absorber support for aerial survey remote sensing

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle damping bracket for aerial survey remote sensing.

Background

To unmanned aerial vehicle support for aerial survey remote sensing that knows, this support is in use, and the fixed structure of commonly used only can use to the unmanned aerial vehicle of same size, and can not dismantle, is unfavorable for accomodating, and is inconvenient in the use, so on the market an urgent need can be to the unmanned aerial vehicle support of different unmanned aerial vehicle adjustment support sizes, refer to patent number: CN202221514787.X, we consider to design an unmanned aerial vehicle support for aerial survey remote sensing for the purpose of increasing convenience.

The existing unmanned aerial vehicle support is in use, has no damping structure, and when suddenly falling, internal parts are damaged due to overlarge impact force, so that the service life of the unmanned aerial vehicle is influenced.

Disclosure of Invention

(one) solving the technical problems

Aiming at the defects of the prior art, the utility model provides the unmanned aerial vehicle shock-absorbing bracket for aerial survey remote sensing, which has the advantages of convenient operation, adjustable supporting size, shock resistance and the like, and solves the problems that the unmanned aerial vehicle with the same size can only be used, can not be disassembled, is unfavorable for storage, is inconvenient to use, has no shock-absorbing structure, causes damage to internal parts due to overlarge impact force when suddenly falling, and affects the service life of the unmanned aerial vehicle.

(II) technical scheme

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle shock absorber support for aerial survey remote sensing, includes the main part, main part upper end surface front end edge fixedly connected with slide bar, slide bar upper end surface is close to right side edge sliding connection has the slider, slider front end surface center department fixedly connected with upper bracket, upper bracket front end surface middle lower department swing joint has the fixed axle, upper bracket front end inner surface is close to upper end department fixedly connected with first spring, first spring rear end surface fixedly connected with limiting plate, main part front end surface is close to left side edge and is seted up flutedly.

Preferably, the center of the outer surface of the lower end of the upper support frame is fixedly connected with a second spring, the outer surface of the lower end of the second spring is fixedly connected with a lower support frame, and the left inner surface of the lower support frame is provided with a sliding groove.

Preferably, the upper support frame and the lower support frame are respectively four, the front upper support frame and the rear upper support frame are respectively fixedly connected with two ends of the same cross rod, the front lower support frame and the rear lower support frame are respectively fixedly connected with two ends of the same cross rod, the number of the grooves is a plurality of, the grooves are respectively uniformly distributed at the left side edge and the right side edge of the outer surfaces of the front end and the rear end of the main body, the upper support frame and the lower support frame are connected to ensure that the upper support frame and the lower support frame provide stable support, and a plurality of grooves are arranged to enable the adjustment of equipment to have more choices.

Preferably, the center of the outer surface of the upper end of the main body is fixedly connected with an interface, the interface corresponds to the upper joint of the unmanned aerial vehicle, the rear end of the fixed shaft is mutually matched with the groove, the unmanned aerial vehicle can be fixedly installed through the interface, and the operation stability is ensured through the mutually matched relationship.

Preferably, the edges of the lower ends of the left and right outer surfaces of the upper support frame are respectively in sliding connection with the sliding grooves, and the sliding connection between the left and right sides of the upper support frame and the sliding grooves ensures that the two sides of the upper support frame synchronously descend in the descending process, so that the upper support frame is prevented from shaking left and right.

Preferably, the length of spout is less than the height of lower carriage, second spring length is long enough, lower carriage lower extreme surface is provided with the cushion, prevents through the length that sets up the spout that upper carriage and lower carriage from producing the collision, prevents through setting up the cushion that the lower carriage from producing too big collision at the in-process of falling to the ground.

Compared with the prior art, the utility model provides the unmanned aerial vehicle damping bracket for aerial survey remote sensing, which has the following beneficial effects:

1. this unmanned aerial vehicle shock absorber support for aerial survey remote sensing, through slide bar, the slider, the upper supporting frame, the fixed axle, limiting plate, first spring isotructure, when the width of needs adjustment support, take out the fixed axle at both ends around with left side and right side, move the upper supporting frame to the position that needs the adjustment, and loosen the fixed axle, at the effect of first spring and limiting plate, the fixed axle is recovered, and the recess that its rear end got into this department is fixed, if need accomodate, only need pull open the fixed axle, take off the upper supporting frame can, convenient operation, support size adjustable.

2. This unmanned aerial vehicle shock absorber support for aerial survey remote sensing, through second spring, lower carriage, spout isotructure, when unmanned aerial vehicle descends suddenly, through the sliding relationship between upper bracket and the lower carriage, remain stable, play cushioning effect through extrusion second spring to reduce the decline speed of upper bracket, prevent that the impact force is too big to cause unmanned aerial vehicle part to damage.

Drawings

FIG. 1 is a schematic diagram of the overall structure of the present utility model;

FIG. 2 is a right side cross-sectional view of the structure of the stationary shaft of the present utility model;

fig. 3 is a front cross-sectional view of the chute structure of the present utility model.

Wherein: 1. a main body; 2. a slide bar; 3. a slide block; 4. an upper support frame; 5. a fixed shaft; 6. a limiting plate; 7. a first spring; 8. a groove; 9. a second spring; 10. a lower support frame; 11. and a sliding groove.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Embodiment 1, as shown in fig. 1-2, an unmanned aerial vehicle shock absorber support for aerial survey remote sensing, which comprises a main body 1, the front end edge of main body 1 upper end surface front end fixedly connected with slide bar 2, slide bar 2 upper end surface is close to right side edge department sliding connection has slider 3, slider 3 front end surface center department fixedly connected with upper bracket 4, upper bracket 4 front end surface middle is near lower department swing joint has fixed axle 5, upper bracket 4 front end inner surface is close to upper end department fixedly connected with first spring 7, first spring 7 rear end outer surface fixedly connected with limiting plate 6, main body 1 front end surface is close to left side edge department and has seted up recess 8, upper bracket 4, lower carriage 10 have four respectively, two upper brackets 4 in front and back respectively with the both ends fixedly connected with of same horizontal pole, the quantity of recess 8 is a plurality of respectively evenly distributed in main body 1 front and rear end surface's left side edge department and right side edge department, 1 front end surface and right side edge department, the upper bracket is close to left side edge department and the corresponding recess 8 of this front end, and the corresponding interface of this front end and rear end of the main body 1, the interface is mutually corresponding to the fixed axle.

The working principle is as follows; in use, the joint on the unmanned aerial vehicle is fixed with the interface at the center of the outer surface of the upper end of the main body 1, when the width of the bracket needs to be adjusted, the fixed shafts 5 at the front end and the rear end of the left side and the right side are pulled out, the upper support frame 4 is moved to the position needing to be adjusted by sliding the sliding block 3 on the sliding rod 2, the fixed shafts 5 are loosened, the first springs 7 enable the positions of the fixed shafts 5 to be restored, the rear ends of the fixed shafts 5 are pushed into the grooves 8 at the positions to be fixed, if the fixed shafts 5 need to be stored, only the fixed shafts 5 are pulled out, the upper support frame 4 is taken down, the fixed shafts 5 are guaranteed not to be pulled out by the limiting plates 6 in the process of pulling the fixed shafts 5, and the fixed shafts 5 are restored by pushing the limiting plates 6 by the first springs 7 in the process of loosening the fixed shafts 5.

In embodiment 2, as shown in fig. 1-3, a second spring 9 is fixedly connected to the center of the outer surface of the lower end of the upper support frame 4, the outer surface of the lower end of the second spring 9 is fixedly connected with a lower support frame, a sliding groove 11 is formed in the left inner surface of the lower support frame 10, the edges of the lower ends of the left outer surface and the right outer surface of the upper support frame 4 are respectively and slidably connected with the sliding groove 11, the length of the sliding groove 11 is smaller than the height of the lower support frame 10, the length of the second spring 9 is long enough, and a soft cushion is arranged on the outer surface of the lower end of the lower support frame 10.

The working principle is as follows; when unmanned aerial vehicle drops suddenly, through the sliding relation of upper support frame 4 and spout 11, guarantee unmanned aerial vehicle's stability in vertical direction to through extrusion second spring 9, make unmanned aerial vehicle's whereabouts obtain buffering, and reduce upper support frame 4's decline speed, prevent that the impact force is too big to cause unmanned aerial vehicle part to damage, this in-process lower support frame 10 contacts ground at first, and reduces through the cushion and collide with.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. Unmanned aerial vehicle shock absorber support for aerial survey remote sensing, including main part (1), its characterized in that: the novel sliding type sliding device is characterized in that a sliding rod (2) is fixedly connected to the front edge of the upper end surface of the main body (1), a sliding block (3) is slidably connected to the upper end surface of the sliding rod (2) close to the right side edge, an upper supporting frame (4) is fixedly connected to the center of the front end surface of the sliding block (3), a fixing shaft (5) is movably connected to the middle of the front end surface of the upper supporting frame (4) and is positioned below, a first spring (7) is fixedly connected to the inner surface of the front end of the upper supporting frame (4) close to the upper end, a limiting plate (6) is fixedly connected to the outer surface of the rear end of the first spring (7), and a groove (8) is formed in the outer surface of the front end of the main body (1) close to the left side edge.

2. The unmanned aerial vehicle shock absorber support for aerial survey remote sensing according to claim 1, wherein: the center of the outer surface of the lower end of the upper supporting frame (4) is fixedly connected with a second spring (9), the outer surface of the lower end of the second spring (9) is fixedly connected with a lower supporting frame (10), and the inner surface of the left side of the lower supporting frame (10) is provided with a sliding groove (11).

3. The unmanned aerial vehicle shock absorber support for aerial survey remote sensing according to claim 1, wherein: the upper support frames (4) and the lower support frames (10) are respectively four, the front upper support frame (4) and the rear upper support frame (4) are respectively and fixedly connected with two ends of the same cross rod, the front lower support frame (10) and the rear lower support frame (10) are respectively and fixedly connected with two ends of the same cross rod, the number of the grooves (8) is a plurality of, and the grooves are respectively and uniformly distributed at the left side edge and the right side edge of the outer surfaces of the front end and the rear end of the main body (1).

4. The unmanned aerial vehicle shock absorber support for aerial survey remote sensing according to claim 1, wherein: the center of the outer surface of the upper end of the main body (1) is fixedly connected with an interface, the interface corresponds to the upper joint of the unmanned aerial vehicle, and the rear end of the fixed shaft (5) is mutually matched with the groove (8).

5. The unmanned aerial vehicle shock absorber support for aerial survey remote sensing according to claim 2, wherein: the edges of the lower ends of the left side and the right side of the outer surface of the upper supporting frame (4) are respectively connected with the sliding groove (11) in a sliding way.

6. The unmanned aerial vehicle shock absorber support for aerial survey remote sensing according to claim 2, wherein: the length of the sliding groove (11) is smaller than the height of the lower supporting frame (10), the length of the second spring (9) is long enough, and a soft cushion is arranged on the outer surface of the lower end of the lower supporting frame (10).